CN107471801A - 一种铝塑膜专用的尼龙薄膜及其制作方法 - Google Patents

一种铝塑膜专用的尼龙薄膜及其制作方法 Download PDF

Info

Publication number
CN107471801A
CN107471801A CN201710825297.9A CN201710825297A CN107471801A CN 107471801 A CN107471801 A CN 107471801A CN 201710825297 A CN201710825297 A CN 201710825297A CN 107471801 A CN107471801 A CN 107471801A
Authority
CN
China
Prior art keywords
nylon
temperature
section
parts
wind speed
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201710825297.9A
Other languages
English (en)
Other versions
CN107471801B (zh
Inventor
肖勇
郭亮
黄银飞
殷红娟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Purple East Nylon Mstar Technology Ltd
Original Assignee
Shanghai Purple East Nylon Mstar Technology Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanghai Purple East Nylon Mstar Technology Ltd filed Critical Shanghai Purple East Nylon Mstar Technology Ltd
Priority to CN201710825297.9A priority Critical patent/CN107471801B/zh
Publication of CN107471801A publication Critical patent/CN107471801A/zh
Application granted granted Critical
Publication of CN107471801B publication Critical patent/CN107471801B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/34Layered products comprising a layer of synthetic resin comprising polyamides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/001Combinations of extrusion moulding with other shaping operations
    • B29C48/0018Combinations of extrusion moulding with other shaping operations combined with shaping by orienting, stretching or shrinking, e.g. film blowing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/92Measuring, controlling or regulating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C55/00Shaping by stretching, e.g. drawing through a die; Apparatus therefor
    • B29C55/02Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets
    • B29C55/10Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets multiaxial
    • B29C55/12Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets multiaxial biaxial
    • B29C55/14Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets multiaxial biaxial successively
    • B29C55/143Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets multiaxial biaxial successively firstly parallel to the direction of feed and then transversely thereto
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/06Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/18Layered products comprising a layer of synthetic resin characterised by the use of special additives
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L77/00Compositions of polyamides obtained by reactions forming a carboxylic amide link in the main chain; Compositions of derivatives of such polymers
    • C08L77/02Polyamides derived from omega-amino carboxylic acids or from lactams thereof
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/10Primary casings; Jackets or wrappings
    • H01M50/116Primary casings; Jackets or wrappings characterised by the material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/54Yield strength; Tensile strength
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558Impact strength, toughness
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/18Oxygen-containing compounds, e.g. metal carbonyls
    • C08K3/24Acids; Salts thereof
    • C08K3/26Carbonates; Bicarbonates
    • C08K2003/265Calcium, strontium or barium carbonate
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/18Oxygen-containing compounds, e.g. metal carbonyls
    • C08K3/24Acids; Salts thereof
    • C08K3/26Carbonates; Bicarbonates
    • C08K2003/267Magnesium carbonate
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

Landscapes

  • Mechanical Engineering (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Polymers & Plastics (AREA)
  • Medicinal Chemistry (AREA)
  • Health & Medical Sciences (AREA)
  • Organic Chemistry (AREA)
  • Electrochemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)
  • Shaping By String And By Release Of Stress In Plastics And The Like (AREA)
  • Laminated Bodies (AREA)

Abstract

本发明公开了一种铝塑膜专用的尼龙薄膜及其制作方法,尼龙薄膜由中间层以及分别复合在中间层上、下表面的表层构成,所述中间层与表层的厚度比为:74‑78:22‑26;所述表层含有如下质量份数的物质:尼龙6 55‑65份,特种尼龙35‑45份,抗粘连剂0.3‑0.7份;所述中间层中含有如下质量份数的物质:尼龙6 55‑65份,特种尼龙35‑45份;所述特种尼龙为PA612、PA610、PA1012中一种或者任意组合。本发明获得了具有拉伸强度以及拉伸率高且均匀的铝塑膜专用尼龙薄膜,具有耐冲深高的优点。

Description

一种铝塑膜专用的尼龙薄膜及其制作方法
技术领域
本发明属于尼龙薄膜技术领域,尤其涉及一种铝塑膜专用的尼龙薄膜及其制作方法。
背景技术
软包装锂离子电池采用同聚合物锂离子电池相类似的铝塑复合膜作为电池的外壳,取代一般锂离子电池的钢制或铝制外壳。这种铝塑复合膜大致可以分为三层:内层为粘结层,多采用聚乙烯或聚丙烯材料,起封口粘结作用;中间层为铝箔,能够防止电池外部水汽的渗入,同时防止内部电解液的渗出;外层为保护层,多采用高熔点的聚酯或尼龙材料,有很强的机械性能,防止外力对电池的损伤,起保护电池的作用。
目前市场上的尼龙薄膜材料,在纵向和横向上的拉伸强度非常不均匀,而且伸长率也非常不均匀,导致铝塑复合膜在固定的压力和速度下冲深,冲深2.5mm-3mm就会冲破。
发明内容
本发明所要解决的技术问题是提供一种纵横向拉伸强度大且均匀、纵横向伸长率大且均匀的铝塑膜专用的尼龙薄膜及其制备方法,以克服现在耐冲深低的不足。
为了解决上述技术问题,本发明采用如下的技术方案:
一种铝塑膜专用的尼龙薄膜,由中间层以及分别复合在中间层上、下表面的表层构成,所述中间层与表层的厚度比为:74-78:22-26;
所述表层含有如下质量份数的物质:
尼龙6 55-65份,
特种尼龙 35-45份,
抗粘连剂 0.3-0.7份;
所述中间层中含有如下质量份数的物质:
尼龙6 55-65份,
特种尼龙 35-45份;
所述特种尼龙为PA612、PA610、PA1012中一种或者任意组合。
所述抗粘连剂为二氧化硅或碳酸钙或碳酸镁。
另外,本发明还提供了一种热铝塑膜专用的尼龙薄膜的制作方法,该制作方法包括如下的步骤:
投料:表层的物质按下列重量比例投入干燥缸中:
尼龙6 55-65份,
特种尼龙 35-45份,所述特种尼龙为MXD6、PA612、PA610中一种或者任意组合,
抗粘连剂 0.3-0.7份,
中间层的物质按下列重量比例投入干燥缸中:
尼龙6 55-65份,
特种尼龙 35-45份;
所述尼龙6和所述特殊尼龙的粘度均为2.8-3.2;
特种尼龙为PA612、PA610、PA1012中一种或者任意组合;
原料干燥:采取蒸汽加热,温度达到90℃后开启真空泵进行干燥,30min后停止真空泵并充入氮气,取样测试水分,当干燥程度达到1000-1100ppm,干燥结束,否则重复干燥;
熔融挤出:原料干燥后进入挤出机,所述挤出机从加料口到挤出口的各段的温度依次为:第一进料段259-261℃,第二进料段269-271℃,第一熔融段274-276℃,第二熔融段279-281℃,第三熔融段279-281℃,第一挤出段274-276℃,第二挤出段269-271℃,第三挤出段269-271℃;原料通过挤出机熔化后,熔体经管道输送至T型模头流出到冷却辊,形成厚片,所述冷却辊的温度为21-23℃,速度为60-61rpm/min;通过调整中间层原料和表层原料的单位时间挤出量实现所述中间层与表层的厚度比为:74-78:22-26;
纵向拉伸:厚片经辊筒输送至纵向拉伸区域后依次进行预热、拉伸和定型,纵向拉伸比为3.1-3.4,拉伸方法为单点拉伸;所述纵向拉伸的预热分两段进行,第一预热段温度为49-51℃,第二预热段温度为57-59℃;所述纵向拉伸的拉伸分两段进行,第一拉伸段温度为61-63℃,第二拉伸段温度也为61-63℃;所述纵向拉伸的定型分两段进行,第一定型段温度为51-53℃,第二定型段温度为44-46℃;
横向拉伸:经纵向拉伸后的厚片进入横向拉伸区域后依次进行预热、拉伸、定型和冷却,横向拉伸比为3.8-4.2;所述横向拉伸的预热分三段进行,第一预热段温度为85~90℃,风速为17-19m/s,第二预热段温度为90~95℃,风速为17-19m/s,第三预热段温度为100~110℃,风速为17-19m/s;所述横向拉伸的拉伸分三段进行,第一拉升段的温度为100-110℃,风速为17-19m/s,第二拉伸段的温度为105-115℃,风速为17-19m/s,第三拉伸段的温度为107-115℃,风速为17-19m/s;所述横向拉伸的定型分七段进行,第一定型段的温度为169-171℃,风速为
12-14m/s,第二至第六定型段的温度均为220-225℃,第二至第五段定型的风速均为12-14m/s,第七定型段的温度为179-181℃,第六和第七定型段的风速均为13-15m/s,所述冷却段的温度为39-41℃,风速为13-15m/s。
通过采用上述技术方案,获得了具有拉伸强度以及拉伸率高且均匀的铝塑膜专用尼龙薄膜,具有耐冲深高的优点。
附图说明
图1为本发明的热铝塑膜专用的尼龙薄膜的结构剖视图。
具体实施方式
如图1所示,本实施例的铝塑膜专用的尼龙薄膜,由中间层100以及分别复合在中间层上、下表面的表层200构成,中间层与表层的厚度比为:25:8。其按照下列工艺制得。
投料:
表层的料按下列重量比投入干燥缸:
尼龙6 60份,
特种尼龙PA610 39.4份,
抗粘连剂二氧化硅 0.6份。
所述中间层中含有如下质量份数的物质:
尼龙6 60份,
特种尼龙PA612 40份。
中间层的料按下列重量比投入干燥缸:
尼龙6 60份,
特种尼龙PA610 40份;
尼龙6和特种尼龙的粘度均为2.8-3.2。
原料干燥:采取蒸汽加热,温度达到90℃后开启真空泵进行干燥,30min后停止真空泵并充入氮气,取样测试水分,当干燥程度达到1000-1100ppm,干燥结束,否则重复干燥;
熔融挤出:
原料干燥后进入挤出机,加料口采用真空保护,真空度稳定在-80kpa,挤出机从加料口到挤出口的各段温度如下表所示:
原料通过挤出机熔化后,熔体经管道输送至T型模头流出到冷却辊,形成厚片,所述冷却辊的温度为22℃,速度为60.5rpm/min。
在本步骤中,通过调整中间层原料和表层原料的单位时间挤出量,即调整各自齿轮泵的转速实现所述中间层与表层的厚度比为25:8,具体地是通过调整各自齿轮泵的转速来实现中间层和表层的厚度比。
纵向拉伸:
厚片经辊筒输送至纵向拉伸区域后依次进行预热、拉伸和定型,完成纵向拉伸。纵向拉伸比为3.1-3.4,拉伸方法为单点拉伸,纵向拉伸的各区段温度设置如下表:
为保证拉升比不变,防止拉伸不均匀,拉伸前后均有压辊压住厚片,压辊压力为0.3-0.5MPa。
横向拉伸:
经纵向拉伸后的厚片进入横向拉伸,依靠链夹夹住边部,链夹运行轨道越来越宽完成拉伸。横向拉升比为3.8-4.2。
横向拉伸分为预热、拉伸、定型、冷却四个区段。
横向拉伸各区段温度和风速设置如下表。
制得的铝塑膜专用的尼龙薄膜,经检测,性能指标如下:
并且还将该铝塑膜专用的尼龙薄膜用来制作铝塑复合膜样品,用样品做耐冲深试验,试验结果为:冲深到达5.0mm,样品不破。
但是,本技术领域中的普通技术人员应当认识到,以上的实施例仅是用来说明本发明,而并非用作为对本发明的限定,只要在本发明的实质精神范围内,对以上所述实施例的变化、变型都将落在本发明的权利要求书范围内。

Claims (4)

1.一种铝塑膜专用的尼龙薄膜,其特征在于:由中间层以及分别复合在中间层上、下表面的表层构成,所述中间层与表层的厚度比为:74-78:22-26;
所述表层含有如下质量份数的物质:
尼龙6 55-65份,
特种尼龙 35-45份,
抗粘连剂 0.3-0.7份;
所述中间层中含有如下质量份数的物质:
尼龙6 55-65份,
特种尼龙 35-45份;
所述特种尼龙为PA612、PA610、PA1012中一种或者任意组合。
2.根据权利要求1所述的铝塑膜专用的尼龙薄膜,其特征在于:所述抗粘连剂为二氧化硅或碳酸钙或碳酸镁。
3.一种热铝塑膜专用的尼龙薄膜的制作方法,其特征在于:该制作方法包括如下的步骤:
投料:表层的物质按下列重量比例投入干燥缸中:
尼龙6 55-65份,
特种尼龙 35-45份,所述特种尼龙为MXD6、PA612、PA610中一种或者任意组合,
抗粘连剂 0.3-0.7份,
中间层的物质按下列重量比例投入干燥缸中:
尼龙6 55-65份,
特种尼龙 35-45份;
特种尼龙为PA612、PA610、PA1012中一种或者任意组合;
原料干燥:采取蒸汽加热,温度达到90℃后开启真空泵进行干燥,30min后停止真空泵并充入氮气,取样测试水分,当干燥程度达到1000-1100ppm,干燥结束,否则重复干燥;
熔融挤出:原料干燥后进入挤出机,所述挤出机从加料口到挤出口的各段的温度依次为:第一进料段259-261℃,第二进料段269-271℃,第一熔融段274-276℃,第二熔融段279-281℃,第三熔融段279-281℃,第一挤出段274-276℃,第二挤出段269-271℃,第三挤出段269-271℃;原料通过挤出机熔化后,熔体经管道输送至T型模头流出到冷却辊,形成厚片,所述冷却辊的温度为21-23℃,速度为60-61rpm/min;通过调整中间层原料和表层原料的单位时间挤出量实现所述中间层与表层的厚度比为:74-78:22-26;
纵向拉伸:厚片经辊筒输送至纵向拉伸区域后依次进行预热、拉伸和定型,纵向拉伸比为3.1-3.4,拉伸方法为单点拉伸;所述纵向拉伸的预热分两段进行,第一预热段温度为49-51℃,第二预热段温度为57-59℃;所述纵向拉伸的拉伸分两段进行,第一拉伸段温度为61-63℃,第二拉伸段温度也为61-63℃;所述纵向拉伸的定型分两段进行,第一定型段温度为51-53℃,第二定型段温度为44-46℃;
横向拉伸:经纵向拉伸后的厚片进入横向拉伸区域后依次进行预热、拉伸、定型和冷却,横向拉伸比为3.8-4.2;所述横向拉伸的预热分三段进行,第一预热段温度为85~90℃,风速为17-19m/s,第二预热段温度为90~95℃,风速为17-19m/s,第三预热段温度为100~110℃,风速为17-19m/s;所述横向拉伸的拉伸分三段进行,第一拉升段的温度为100-110℃,风速为17-19m/s,第二拉伸段的温度为105-115℃,风速为17-19m/s,第三拉伸段的温度为107-115℃,风速为17-19m/s;所述横向拉伸的定型分七段进行,第一定型段的温度为169-171℃,风速为12-14m/s,第二至第六定型段的温度均为220-225℃,第二至第五段定型的风速均为12-14m/s,第七定型段的温度为179-181℃,第六和第七定型段的风速均为13-15m/s,所述冷却段的温度为39-41℃,风速为13-15m/s。
4.根据权利要求3所述的热铝塑膜专用的尼龙薄膜的制作方法,其特征在于:所述抗粘连剂为二氧化硅或碳酸钙或碳酸镁。
CN201710825297.9A 2017-09-14 2017-09-14 一种铝塑膜专用的尼龙薄膜及其制作方法 Active CN107471801B (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710825297.9A CN107471801B (zh) 2017-09-14 2017-09-14 一种铝塑膜专用的尼龙薄膜及其制作方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710825297.9A CN107471801B (zh) 2017-09-14 2017-09-14 一种铝塑膜专用的尼龙薄膜及其制作方法

Publications (2)

Publication Number Publication Date
CN107471801A true CN107471801A (zh) 2017-12-15
CN107471801B CN107471801B (zh) 2020-02-14

Family

ID=60584355

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710825297.9A Active CN107471801B (zh) 2017-09-14 2017-09-14 一种铝塑膜专用的尼龙薄膜及其制作方法

Country Status (1)

Country Link
CN (1) CN107471801B (zh)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112143220A (zh) * 2020-09-10 2020-12-29 厦门长塑实业有限公司 一种高爽滑聚酰胺母粒、聚酰胺薄膜及其制备方法
CN112226076A (zh) * 2020-09-10 2021-01-15 厦门长塑实业有限公司 一种超高爽滑聚酰胺母粒、聚酰胺薄膜及其制备方法
CN114261166A (zh) * 2021-12-28 2022-04-01 上海紫东尼龙材料科技有限公司 一种耐高温尼龙薄膜及其制作方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090130407A1 (en) * 2005-05-27 2009-05-21 Showa Denko Packaging Co. Packaging material for battery case and battery case
CN101663774A (zh) * 2007-05-21 2010-03-03 昭和电工包装株式会社 电池外壳用包装材料及电池用外壳
JP2011162702A (ja) * 2010-02-12 2011-08-25 Kohjin Co Ltd 冷間成形用二軸延伸ナイロンフィルム
CN106832907A (zh) * 2017-03-09 2017-06-13 上海紫东化工材料有限公司 热收缩率达到8‑10%的高收缩双向拉伸尼龙6薄膜及其制作方法

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090130407A1 (en) * 2005-05-27 2009-05-21 Showa Denko Packaging Co. Packaging material for battery case and battery case
CN101663774A (zh) * 2007-05-21 2010-03-03 昭和电工包装株式会社 电池外壳用包装材料及电池用外壳
JP2011162702A (ja) * 2010-02-12 2011-08-25 Kohjin Co Ltd 冷間成形用二軸延伸ナイロンフィルム
CN106832907A (zh) * 2017-03-09 2017-06-13 上海紫东化工材料有限公司 热收缩率达到8‑10%的高收缩双向拉伸尼龙6薄膜及其制作方法

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112143220A (zh) * 2020-09-10 2020-12-29 厦门长塑实业有限公司 一种高爽滑聚酰胺母粒、聚酰胺薄膜及其制备方法
CN112226076A (zh) * 2020-09-10 2021-01-15 厦门长塑实业有限公司 一种超高爽滑聚酰胺母粒、聚酰胺薄膜及其制备方法
CN114261166A (zh) * 2021-12-28 2022-04-01 上海紫东尼龙材料科技有限公司 一种耐高温尼龙薄膜及其制作方法

Also Published As

Publication number Publication date
CN107471801B (zh) 2020-02-14

Similar Documents

Publication Publication Date Title
CN107471801A (zh) 一种铝塑膜专用的尼龙薄膜及其制作方法
CN107652670B (zh) 一种增韧型双向拉伸聚酰胺薄膜及其制备方法
CN106832907B (zh) 热收缩率达到8-10%的高收缩双向拉伸尼龙6薄膜及其制作方法
CN104589749B (zh) 高阻隔双向拉伸聚乙烯薄膜及其制备方法
CN106183292B (zh) 三层共挤快速双向拉伸宽幅聚乙烯复合薄膜及其制备方法
WO2015138096A1 (en) Improved biaxially oriented metallocene linear low density polyethylene film, method and resin composition for same
CN106029376B (zh) 制造聚合物薄膜的方法和共挤出薄膜
CN210526002U (zh) 一种耐高温高阻隔聚烯烃复合膜
JP2017515952A5 (zh)
CN108129736B (zh) 耐高温pe膜及其制备方法和包含耐高温pe膜的包装袋
CN101528441A (zh) 双轴拉伸尼龙薄膜、层压包装材料及双轴拉伸尼龙薄膜的制造方法
CN101293413A (zh) 高强度减量化聚酯薄膜及其制备方法
CN104527189A (zh) 一种在线双层复合塑料吹塑膜片及其制造方法
CN103802424B (zh) 一种聚乙烯强力交叉复合膜及其生产工艺
CN101844643B (zh) 用于背胶袋的改性聚丙烯薄膜及其制备方法
CN109093978A (zh) 一种高拉伸倍数的薄膜及其生产方法
CN105235336B (zh) 一种耐低温的双向拉伸聚丙烯薄膜及其制备方法
KR20200077666A (ko) 식품 포장용 필름
CN107972343B (zh) 聚丙烯复合材料和聚丙烯自增强复合材料及其制备方法
CN106280306B (zh) 可热封高阻隔包装膜
CN101439581B (zh) 一种易撕型塑料薄膜的制造设备
CN110229416A (zh) 一种高强度抗紫外缓冲气垫聚乙烯薄膜及其制备方法
CN103753825A (zh) 多层共挤低温收缩聚烯烃热收缩膜的生产方法
CN106626654A (zh) 聚烯烃双向拉伸膜及其制备方法
CN103358560A (zh) 一种多层共挤低温收缩聚烯烃热收缩膜的生产方法

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant